View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60470U 26145.43129446 +.00000000 +00000-0 +22897-3 0 00002
2 60470 97.3755 224.7805 0001200 38.8654 321.2673 15.30672178 04
| Epoch (UTC): | 25 May 2026 10:21:03 |
| Eccentricity: | 0.0001200 |
| inclination: | 97.3755° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 224.7805° |
| argument of perigee: | 38.8654° |
| revolutions per day: | 15.30672178 |
| mean anomaly at epoch: | 321.2673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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